WO2011089414A3 - Sandwich panels for aerospace structural application - Google Patents
Sandwich panels for aerospace structural application Download PDFInfo
- Publication number
- WO2011089414A3 WO2011089414A3 PCT/GB2011/050054 GB2011050054W WO2011089414A3 WO 2011089414 A3 WO2011089414 A3 WO 2011089414A3 GB 2011050054 W GB2011050054 W GB 2011050054W WO 2011089414 A3 WO2011089414 A3 WO 2011089414A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- sandwich panels
- structural application
- aerospace structural
- face
- core material
- Prior art date
Links
- 239000011162 core material Substances 0.000 abstract 2
- 239000000853 adhesive Substances 0.000 abstract 1
- 230000001070 adhesive effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/024—Woven fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
- B32B5/026—Knitted fabric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/22—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
- B32B5/24—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
- B32B5/26—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer another layer next to it also being fibrous or filamentary
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0276—Polyester fibres
- B32B2262/0284—Polyethylene terephthalate [PET] or polybutylene terephthalate [PBT]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2264/00—Composition or properties of particles which form a particulate layer or are present as additives
- B32B2264/02—Synthetic macromolecular particles
- B32B2264/0214—Particles made of materials belonging to B32B27/00
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/02—Cellular or porous
- B32B2305/024—Honeycomb
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/18—Fabrics, textiles
- B32B2305/182—Fabrics, textiles knitted
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/10—Fibres of continuous length
- B32B2305/18—Fabrics, textiles
- B32B2305/188—Woven fabrics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2305/00—Condition, form or state of the layers or laminate
- B32B2305/72—Cured, e.g. vulcanised, cross-linked
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/542—Shear strength
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/718—Weight, e.g. weight per square meter
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2313/00—Elements other than metals
- B32B2313/04—Carbon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2363/00—Epoxy resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/10—Scrim [e.g., open net or mesh, gauze, loose or open weave or knit, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP20110700758 EP2525969A2 (en) | 2010-01-20 | 2011-01-17 | Sandwich panels for aerospace structural application |
CA2786631A CA2786631C (en) | 2010-01-20 | 2011-01-17 | Sandwich panels for aerospace structural applications |
RU2012135472/05A RU2545370C2 (en) | 2010-01-20 | 2011-01-17 | Sandwich panel |
CN2011800066408A CN102712164A (en) | 2010-01-20 | 2011-01-17 | Sandwich panels for aerospace structural application |
BR112012014359-0A BR112012014359B1 (en) | 2010-01-20 | 2011-01-17 | uncured sandwich structural panel, sandwich structural panel comprising the uncured sandwich structural panel and aircraft structural panel comprising the sandwich structural panel |
JP2012549415A JP5838170B2 (en) | 2010-01-20 | 2011-01-17 | Sandwich panel |
US13/521,808 US9314992B2 (en) | 2010-01-20 | 2011-01-17 | Sandwich panels |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1000870A GB2477091A (en) | 2010-01-20 | 2010-01-20 | Structureal laminate comprising face sheets, core and open-structured sheet |
GB1000870.4 | 2010-01-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2011089414A2 WO2011089414A2 (en) | 2011-07-28 |
WO2011089414A3 true WO2011089414A3 (en) | 2012-05-31 |
Family
ID=42045790
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/GB2011/050054 WO2011089414A2 (en) | 2010-01-20 | 2011-01-17 | Sandwich panels |
Country Status (9)
Country | Link |
---|---|
US (1) | US9314992B2 (en) |
EP (1) | EP2525969A2 (en) |
JP (2) | JP5838170B2 (en) |
CN (1) | CN102712164A (en) |
BR (1) | BR112012014359B1 (en) |
CA (1) | CA2786631C (en) |
GB (1) | GB2477091A (en) |
RU (1) | RU2545370C2 (en) |
WO (1) | WO2011089414A2 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3006625B1 (en) * | 2013-06-06 | 2015-06-19 | Stratifies | COMPOSITE PANEL FOR FLOORS OR WALL CLADDING ELEMENTS, AND METHOD FOR MANUFACTURING SUCH PANEL |
US20150239205A1 (en) * | 2014-02-25 | 2015-08-27 | GM Global Technology Operations LLC | Composite material and methods of making and using the same |
RU2621338C2 (en) * | 2015-07-28 | 2017-06-02 | Общество с ограниченной ответственностью "Рейма индастриз" | Method for producing multilayer composite structural materials of sandwich type |
CN105332982B (en) * | 2015-11-26 | 2018-04-13 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of aircraft metal resistant cementing structure product weight losing method |
US10273935B2 (en) | 2016-01-15 | 2019-04-30 | General Electric Company | Rotor blades having structural skin insert and methods of making same |
US10800129B2 (en) | 2017-01-24 | 2020-10-13 | Bell Textron Inc. | Honeycomb core sandwich panels |
JP6854880B2 (en) * | 2017-03-23 | 2021-04-07 | 帝人株式会社 | Self-adhesive prepreg and its manufacturing method |
US10391735B2 (en) | 2017-04-07 | 2019-08-27 | Hexcel Corporation | Use of fibrous veils to reduce core crush in honeycomb sandwich structures |
FR3089854B1 (en) | 2018-12-18 | 2022-02-04 | Saint Gobain Performance Plastics France | METHOD FOR PREPARING A COMPOSITE MATERIAL IN THE FORM OF A SANDWICH |
WO2021078400A1 (en) * | 2019-10-25 | 2021-04-29 | Toyota Motor Europe | Composite panel and method for manufacturing the same |
RU2723856C1 (en) * | 2019-11-12 | 2020-06-17 | Общество с ограниченной ответственностью «АЛ-СЕРВИС» | Method of making composite bumper for ground vehicle |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USH47H (en) * | 1985-05-15 | 1986-04-01 | E. I. Du Pont De Nemours And Company | Panel with aramid honeycomb core |
US4879152A (en) * | 1989-02-15 | 1989-11-07 | Green Patrick H | Composite panel structure |
US4963408A (en) * | 1988-06-13 | 1990-10-16 | Mono-Lite Corporation | Structural unitary composite laminate structure and method for making same |
US20080160860A1 (en) * | 2004-03-02 | 2008-07-03 | Toray Industries, Inc. | Epoxy Resin Composition for Fiber-Reinforced Composite Material, Prepreg, and Fiber-Reinforced Composite Material |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4954382A (en) | 1988-11-01 | 1990-09-04 | American Cyanamid Company | Interleaf layer in fiber reinforced resin laminate composites |
CN1087858A (en) * | 1992-12-10 | 1994-06-15 | 谢钧谟 | Wire, band reinforced plastics multilayer materials |
WO1997028210A1 (en) | 1996-02-02 | 1997-08-07 | Toray Industries, Inc. | Resin compositions for fiber-reinforced composite materials and processes for producing the same, prepregs, fiber-reinforced composite materials, and honeycomb structures |
DE69610830T2 (en) * | 1996-07-22 | 2001-05-17 | Hexcel Corp | Honeycomb core materials with particulate reinforcement |
JP4342620B2 (en) * | 1998-12-02 | 2009-10-14 | 富士重工業株式会社 | Method for forming honeycomb sandwich structure composite panel |
US6440257B1 (en) | 2000-05-18 | 2002-08-27 | Hexcel Corporation | Self-adhesive prepreg face sheets for sandwich panels |
US6508910B2 (en) * | 2000-05-18 | 2003-01-21 | Hexcel Corporation | Self-adhesive prepreg face sheet for sandwich panels |
US20040067705A1 (en) | 2002-10-07 | 2004-04-08 | National Research Council Of Canada | Process of bonding and composites made therefrom |
US20050257887A1 (en) | 2004-05-24 | 2005-11-24 | Tsotsis Thomas K | Method and apparatus for melt-bonded materials for tackification of dry fabric preforms |
KR20060011868A (en) * | 2003-05-15 | 2006-02-03 | 헌트스만 인터내셔날, 엘엘씨 | Polyisocyanate-based adhesive formulation for use in sandwich panels |
CN100506908C (en) * | 2004-03-02 | 2009-07-01 | 东丽株式会社 | Epoxy resin composition for fiber-reinforced composite material, prepreg and fiber-reinforced composite material |
DK1595689T3 (en) | 2004-05-11 | 2007-05-14 | Hexcel Holding Gmbh | Prepregs for use in building structures of composite materials and methods for their manufacture |
US7507461B2 (en) * | 2004-09-01 | 2009-03-24 | Hexcel Corporation | Edge coating for honeycomb used in panels with composite face sheets |
US20060048881A1 (en) | 2004-09-08 | 2006-03-09 | Evans Richard B | Laser-assisted placement of veiled composite material |
JP5081812B2 (en) | 2005-05-09 | 2012-11-28 | サイテク・テクノロジー・コーポレーシヨン | Resin soluble thermoplastic veil for composite materials |
EP1829674B1 (en) * | 2005-06-08 | 2018-11-28 | Kabushiki Kaisha Shizuka | Sandwich panel including honeycomb structure body and method of producing the sandwich panel |
US7601654B2 (en) * | 2006-03-30 | 2009-10-13 | Honeywell International Inc. | Molded ballistic panel with enhanced structural performance |
EP2067592B1 (en) | 2006-09-28 | 2020-07-15 | Toray Industries, Inc. | Process for producing composite prepreg base, layered base, and fiber-reinforced plastic |
US9511571B2 (en) | 2007-01-23 | 2016-12-06 | The Boeing Company | Composite laminate having a damping interlayer and method of making the same |
UA29467U (en) * | 2007-10-09 | 2008-01-10 | Юлія Сергіївна Зуб | Trio, medicinal rug |
-
2010
- 2010-01-20 GB GB1000870A patent/GB2477091A/en not_active Withdrawn
-
2011
- 2011-01-17 JP JP2012549415A patent/JP5838170B2/en active Active
- 2011-01-17 CA CA2786631A patent/CA2786631C/en not_active Expired - Fee Related
- 2011-01-17 US US13/521,808 patent/US9314992B2/en active Active
- 2011-01-17 BR BR112012014359-0A patent/BR112012014359B1/en not_active IP Right Cessation
- 2011-01-17 EP EP20110700758 patent/EP2525969A2/en not_active Withdrawn
- 2011-01-17 CN CN2011800066408A patent/CN102712164A/en active Pending
- 2011-01-17 RU RU2012135472/05A patent/RU2545370C2/en active
- 2011-01-17 WO PCT/GB2011/050054 patent/WO2011089414A2/en active Application Filing
-
2015
- 2015-07-16 JP JP2015142163A patent/JP5972430B2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USH47H (en) * | 1985-05-15 | 1986-04-01 | E. I. Du Pont De Nemours And Company | Panel with aramid honeycomb core |
US4963408A (en) * | 1988-06-13 | 1990-10-16 | Mono-Lite Corporation | Structural unitary composite laminate structure and method for making same |
US4879152A (en) * | 1989-02-15 | 1989-11-07 | Green Patrick H | Composite panel structure |
US20080160860A1 (en) * | 2004-03-02 | 2008-07-03 | Toray Industries, Inc. | Epoxy Resin Composition for Fiber-Reinforced Composite Material, Prepreg, and Fiber-Reinforced Composite Material |
Also Published As
Publication number | Publication date |
---|---|
CN102712164A (en) | 2012-10-03 |
CA2786631C (en) | 2017-11-07 |
RU2545370C2 (en) | 2015-03-27 |
WO2011089414A2 (en) | 2011-07-28 |
US20120301665A1 (en) | 2012-11-29 |
US9314992B2 (en) | 2016-04-19 |
JP5838170B2 (en) | 2016-01-06 |
GB2477091A (en) | 2011-07-27 |
BR112012014359B1 (en) | 2020-10-27 |
JP2016040122A (en) | 2016-03-24 |
EP2525969A2 (en) | 2012-11-28 |
BR112012014359A2 (en) | 2016-09-06 |
RU2012135472A (en) | 2014-02-27 |
CA2786631A1 (en) | 2011-07-28 |
JP5972430B2 (en) | 2016-08-17 |
GB201000870D0 (en) | 2010-03-10 |
JP2013517167A (en) | 2013-05-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2011089414A3 (en) | Sandwich panels for aerospace structural application | |
WO2015026421A3 (en) | Septumization of honeycomb sandwiches | |
WO2010066692A3 (en) | Core for composite laminated article and manufacture thereof | |
WO2012051531A3 (en) | Non-planar composite structural panel | |
EP4275886A3 (en) | Laminated glazing | |
WO2011088871A3 (en) | Sandwich component and method for the production thereof | |
GB0912015D0 (en) | Stringer | |
MX2009007711A (en) | Improved flooring panels. | |
EP2483076A4 (en) | Composite cores and panels | |
WO2009066036A3 (en) | Cellular-core structure for an acoustic panel | |
WO2008129281A3 (en) | Insulating panel | |
WO2013035995A3 (en) | Method for manufacturing curved-surface display | |
MX355229B (en) | Ceiling panels made from corrugated cardboard. | |
WO2010080988A3 (en) | A method for fabricating thin touch sensor panels | |
PL2115234T3 (en) | Panel and relative manufacturing system and method | |
MX340430B (en) | Solar mirror panels and their manufacture. | |
WO2012046886A3 (en) | Laminate immobilizing jig, laminate assembly manufacturing system, and manufacturing method for laminate assembly | |
WO2012030494A3 (en) | Method for manufacturing an image display device | |
CA3007452C (en) | Enthalpy exchanger | |
WO2014118538A3 (en) | Structural assembly joint | |
TWI456291B (en) | Liquid crystal panel manufacturing method and manufacturing system | |
WO2013074174A3 (en) | Aircraft structure with means for reducing the risk of disbonding in areas of different strain | |
MX2021006608A (en) | Open area core sandwich structure assembly with vehicle exterior surface gloss. | |
RU2014114646A (en) | INTERMEDIATE ACOUSTIC SHELL AND ITS APPLICATION | |
GB201000124D0 (en) | Improved structural sandwich panel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 201180006640.8 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 11700758 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2786631 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: 13521808 Country of ref document: US |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012549415 Country of ref document: JP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2011700758 Country of ref document: EP |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012135472 Country of ref document: RU |
|
REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112012014359 Country of ref document: BR |
|
ENP | Entry into the national phase |
Ref document number: 112012014359 Country of ref document: BR Kind code of ref document: A2 Effective date: 20120613 |